View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 07364U 26131.80876551 +.00000000 +00000-0 -22361-4 0 00005
2 07364 81.2320 239.9099 0049886 9.9777 350.2370 14.06451450 03
| Epoch (UTC): | 11 May 2026 19:24:37 |
| Eccentricity: | 0.0049886 |
| inclination: | 81.2320° |
| perigee height: | 835 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 239.9099° |
| argument of perigee: | 9.9777° |
| revolutions per day: | 14.06451450 |
| mean anomaly at epoch: | 350.2370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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